View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 22276U 26158.24787603 +.00000000 +00000-0 +22166-3 0 00001
2 22276 20.2862 10.1560 0049654 228.4623 131.1537 14.96278950 01
| Epoch (UTC): | 07 June 2026 05:56:56 |
| Eccentricity: | 0.0049654 |
| inclination: | 20.2862° |
| perigee height: | 544 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 10.1560° |
| argument of perigee: | 228.4623° |
| revolutions per day: | 14.96278950 |
| mean anomaly at epoch: | 131.1537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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